| Edition |
2nd ed. |
| Description |
xxi, 793 p. : ill. |
| Series |
AIAA education series |
|
AIAA education series.
|
| Bibliography |
Includes bibliographical references and index. |
| Contents |
Particle kinematics -- Newtonian mechanics -- Rigid body kinematics -- Eulerian mechanics -- Generalized methods of analytical dynamics -- Variational methods in analytical dynamics -- Hamilton's generalized formulations of analytical dynamics -- Nonlinear spacecraft stability and control -- Classical two-body problem -- Restricted three-body problem -- Gravitational potential field models -- Perturbation methods -- Transfer orbits -- Spacecraft formation flying -- Appendix A. Transport theorem derivation using linear algebra -- Appendix B. Various Euler angle transformations -- Appendix C. MRP identity proof -- Appendix D. Conic section transformations -- Appendix E. Numerical subroutines library -- Appendix F. First-order mapping between mean and osculating orbit elements -- Appendix G. Direct linear mapping between Cartesian Hill frame coordinates and orbit element differences -- Appendix H. Hamel coefficients for the rotational motion of a rigid body. |
| Reproduction |
Electronic reproduction. Ann Arbor, MI : ProQuest, 2015. Available via World Wide Web. Access may be limited to ProQuest affiliated libraries. |
| Subject |
Celestial mechanics.
|
|
Differentiable dynamical systems.
|
|
Orbital mechanics.
|
|
Space vehicles -- Control systems.
|
| Genre/Form |
Electronic books.
|
| Added Author |
Junkins, John L.
|
|
ProQuest (Firm)
|
| ISBN |
9781600867217 (alk. paper) |
|
1600867219 (alk. paper) |
|
9781600867224 (electronic bk.) |
|
